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INS-U-OEM

GPS-Aided OEM INS with Air Data Computer

The Inertial Labs GPS-Aided Inertial Navigation System (INS-U-OEM) is OEM version of new generation, fully-integrated, combined GPS, GLONASS, GALILEO, QZSS and BEIDOU GNSS and high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted. Horizontal and Vertical Position, Velocity and Orientation are determined with high accuracy for both motionless and dynamic applications.

Inertial Labs
Paeonian Springs, US

Description

  • INS, AHRS and ADC (Air Data Computer) output data
  • Multi frequency and Multi constellations GNSS Receiver
  • GPS, GLONASS, GALILEO, QZSS and BEIDOU GNSS
  • Designed for fixed-wing and multi-rotor Aerial Platforms
  • Two Barometers for Indicated Airspeed
  • Position accuracy = 1 cm (RTK)
  • Heading accuracy = 0.3 deg (RTK, Dynamic)
  • Pitch & Roll accuracy = 0.1 deg (RTK, Dynamic)
  • Gyro-compensated, embedded Fluxgate magnetic compass
  • Optional external Stand-Alone Magnetic Compass
  • Small Size, light weight, low power • Affordable price

The Inertial Labs INS-U-OEM utilizes advanced single antenna GNSS receiver, two barometers, magnetometers, 3-axes each of calibrated in full operational temperature range Advanced MEMS Accelerometers and Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure.

INS-U-OEM contains Inertial Labs new on-board sensors fusion filter, state-of-the-art navigation and guidance algorithms and calibration software.

KEY FEATURES, BENEFITS & FUNCTIONALITY

  • Commercially exportable GPS-Aided Inertial Navigation System

  • 3-in-1 strapdown system: INS + AHRS + ADC (Air Data Computer)

  • Embedded in-flight calibration

  • UBlox ZED-F9P F9 High Precision GNSS Module

  • Small size & light weight & low power

  • GPS, GLONASS, GALILEO, BEIDOU, QZSS, RTK supported signals

  • Total and static pressure sensors for calculating Indicated Airspeed

  • Embedded or External Inertial Labs Magneto-Inductive and Mini-Fluxgate

    magnetometers (compass)

  • GNSS measurements and IMU raw data for post-processing

  • Advanced, extendable, embedded Kalman Filter-based sensor fusion algorithms

  • State-of-the-art algorithms for different dynamic motions of Helicopters, and UAV

Do you have questions about this product?

  • Questions about price, availability, and/or retailers
  • Questions about technical specifications and usage
  • Questions about suitability for your project or application

Specifications

Other specifications

Export restrictions

ITAR Free

Graphical user interface

Y

Typical application

Fixed-wing, VTOL UAV

Distinguishable features

Low cost, Air Data Computer (ADC)

Environmental

Non-operating shock tolerance [g]

3000

Operating shock tolerance [g]

1500

Min. operating temperature [°C]

-40

Max. operating temperature [°C]

85

Max. rotation speed [deg/s]

950

Software

Name

GUI Software

Filtering

Y

Adaptable filter strength

Kalman

Adaptable input signals

Y

Integrity monitoring of position input

Y

Integrity monitoring of log input

Y

Max. number of position input signals

10

Max. number of log input signals

10

Maximum latency of log input [ms]

3

Maximum latency of position input [ms]

3

Uncertainty indicators given in output

Yes

Uncertainty of time stamp for output [ms]

0.02

GNSS aided uncertainty

Heading [deg]

0.3

Pitch [deg]

0.05

Roll [deg]

0.05

General

Type of application

Air

Year of initial development

2020

Height [mm]

19.9

Width [mm]

37.2

Length [mm]

65

Weight [kg]

0.1

Min. Voltage (DC)

5

Max. Voltage (DC)

32

Power consumption [W]

1

Mean time between failures [hr]

100000

Type of accelerometer

MEMS

Type of gyro

MEMS

Removable from base plate

N

Moving parts

N

GNSS Positioning Sensor

Number of integrated GNSS receivers and antenna ports

1

No. channels p receiver

184

Tracked satellite signals

All Constellations

SBAS differential signals

Yes

RTK Network Compatibility

Yes

Update rate [ Hz ]

200

Cold start [ seconds ]

50

Hot start [ seconds ]

30

Data formats

NMEA formats

NMEA 0183

RTCM

Y

Other

Binary, ASCII

Inertial Measurement Unit

Accelerometer bias [µ-g]

2

gyro bias [deg/hr]

2

Calibration procedure

In-fligth

GNSS positional accuracy

Horizontal Position Accuracy [ RMS in cm ]

150

Horizontal Position Accuracy (RTK) [ RMS in cm ]

1

Documents

Brochure
INS-U-OEM_Datasheet_rev-2.8_Oct_2023.pdf
670.31 KB
INS-U-OEM_Datasheet_rev-2.8_Oct_2023.pdf

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